Enroute Climb Gradient - Cirrus SR22 Pilot Operating Handbook

Cirrus Design
SR22

Enroute Climb Gradient

Conditions:
• Power ....................................................................................................Full Throttle
• Mixture .......................................................................................................Full Rich
• Flaps .......................................................................................................... 0% (UP)
• Airspeed .....................................................................................Best Rate of Climb
Climb Gradients shown are the gain in altitude for the horizontal distance
traversed expressed as Feet per Nautical Mile.
Fuel flow must be set to the placarded limit for all takeoffs and climbs.
Cruise climbs or short duration climbs are permissible at best power as long
as altitudes and temperatures remain within those specified in the table.
For operation in air colder than this table provides, use coldest data shown.
For operation in air warmer than this table provides, use caution.
Weight Press
Altitude
LB FT
SL
2000
4000
6000
3600 8000
10000
12000
14000
16000
SL
2000
4000
6000
2900 8000
10000
12000
14000
16000
P/N 13772-004 P/N 13772-004
Revision 1
• Note •
Climb CLIMB GRADIENT - Feet per Nautical Mile
Speed
-20
KIAS
108 769
106 685
104 603
102 525
101 448
99 375
98 303
96 234
94 168
101 1130
100 1015
99 905
98 800
97 699
96 603
95 610
94 422
93 337
Temperature ~°C
0 20
730 691
647 609
567 531
489 454
414 381
341 309
271 241
204 174
138 110
1078 1026
965 915
857 809
753 708
654 611
560 518
469 429
382 344
299 263
Section 5
Performance Data
40 50
653 635
573 555
496 479
421 405
349 333
279 264
211 197
146 133
84 71
975 951 1039
867 843
763 741
664 642
569 548
478 458
391 372
308 290
229 212
ISA
701
626
554
484
415
349
285
223
163
937
840
746
656
570
487
407
331
5-19 5-19